Call Number (LC) Title Results
NAS 1.15:4193 In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack 1
NAS 1.15:4194 Close-range photogrammetric measurement of static defections for an aeroelastic supercritical wing 1
NAS 1.15:4195 Evaluation of composite components on the Bell 206L and Sikorsky S-76 helicopters 1
NAS 1.15:4196 Advanced technology needs for a global change science program perspective of the Langley Research Center / 1
NAS 1.15:4197 Video camera system for locating bullet holes in targets at a ballistics range 1
NAS 1.15:4198 A linearly controlled direct-current power source for high-current inductive loads in a magnetic suspension wind tunnel 1
NAS 1.15:4199 Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects 1
NAS 1.15:4200 Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform 1
NAS 1.15:4201 Aerodynamic performance of a 0.27-scale model of an AH-64 helicopter with baseline and alternate rotor blade sets 1
NAS 1.15:4202 Space Station Freedom environmental control and life support system (ECLSS) phase III simplified integrated test trace contaminant control subsystem performance 1
NAS 1.15:4203 Collision forces for compliant projectiles 1
NAS 1.15:4204 Space Station Freedom environmental control and life support system phase III simplified integrated test detailed report 1
NAS 1.15:4206 Geometric programming prediction of design trends for OMV protective structures 1
NAS 1.15:4207 Propulsion system/flight control integration and optimization flight evaluation and technology transition / 1
NAS 1.15:4208 Using minimal spanning trees to compare the reliability of network topologies 1
NAS 1.15:4209 Three-dimensional cavity flow fields at subsonic and transonic speeds 1
NAS 1.15:4212 Single launch lunar habitat derived from NSTS external tank 1
NAS 1.15:4213 Data base architecture for instrument characteristics critical to spacecraft conceptual design 1
NAS 1.15:4214 Cyclic hot firing of tungsten-wire-reinforced, copper-lined thrust chambers 1
NAS 1.15:4216 A preliminary evaluation of an F100 engine parameter estimation process using flight data 1